UA29516C2 - method of assembly, preparation, transport to launching site and launching of rockets - Google Patents
method of assembly, preparation, transport to launching site and launching of rocketsInfo
- Publication number
- UA29516C2 UA29516C2 UA97115700A UA97115700A UA29516C2 UA 29516 C2 UA29516 C2 UA 29516C2 UA 97115700 A UA97115700 A UA 97115700A UA 97115700 A UA97115700 A UA 97115700A UA 29516 C2 UA29516 C2 UA 29516C2
- Authority
- UA
- Ukraine
- Prior art keywords
- rocket
- launching
- preparation
- assembly
- rockets
- Prior art date
Links
- 238000000034 method Methods 0.000 title abstract 3
- 235000015842 Hesperis Nutrition 0.000 title abstract 2
- 235000012633 Iberis amara Nutrition 0.000 title abstract 2
- 238000005452 bending Methods 0.000 abstract 2
- 239000000446 fuel Substances 0.000 abstract 2
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B35/00—Vessels or similar floating structures specially adapted for specific purposes and not otherwise provided for
- B63B35/003—Vessels or similar floating structures specially adapted for specific purposes and not otherwise provided for for transporting very large loads, e.g. offshore structure modules
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B1/00—Hydrodynamic or hydrostatic features of hulls or of hydrofoils
- B63B1/02—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving lift mainly from water displacement
- B63B1/10—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving lift mainly from water displacement with multiple hulls
- B63B1/107—Semi-submersibles; Small waterline area multiple hull vessels and the like, e.g. SWATH
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/002—Launch systems
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G5/00—Ground equipment for vehicles, e.g. starting towers, fuelling arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
- F41F3/042—Rocket or torpedo launchers for rockets the launching apparatus being used also as a transport container for the rocket
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G5/00—Ground equipment for vehicles, e.g. starting towers, fuelling arrangements
- B64G2005/005—Systems for launching spacecraft from a platform at sea
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Combustion & Propulsion (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- General Physics & Mathematics (AREA)
- Astronomy & Astrophysics (AREA)
- General Engineering & Computer Science (AREA)
- Fluid Mechanics (AREA)
- Transportation (AREA)
- Automatic Assembly (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
Винахід стосується способу збирання, підготовки, транспортування на стартову позицію та запуску великих ракет, в якому ракета складається з декількох модулів та корисного вантажу, який повинен бути виведений у космос. Спосіб полягає в тому, що збирання, підготовка та транспортування на стартову позицію ракети, що складається з декількох модулів та корисного вантажу, що виводиться у космос, виконують при горизонтальній орієнтації основної осі ракети. Складнощі, обумовлені впливом значних сил та згинаючих моментів у результаті дії ваги палива, вирішуються частково за рахунок того, що ракета укладається в одне або декілька спеціально пристосованих гнізд або сідел, по яким вага розподіляється таким чином, що згинаючі моменти скорочуються, а частково за рахунок того, що значна частина палива заливається після того, як ракета буде піднята у вертикальне положення. Потім повністю зібрана ракета, вісь якої розташована все ще горизонтально, переноситься на плавучу конструкцію. Плавуча конструкція пропливає, відстань, що залишилась до стартової позиції, де ракета підіймається у вертикальне положення і запускається.The invention relates to a method of assembling, preparing, transporting to the starting position and launching large rockets, in which the rocket consists of several modules and a payload to be launched into space. The method consists in the fact that the assembly, preparation and transportation to the launch position of the rocket, consisting of several modules and payload, launched into space, is performed with a horizontal orientation of the main axis of the rocket. The difficulties due to the influence of significant forces and bending moments as a result of the weight of the fuel are solved in part by the fact that the rocket is placed in one or more specially adapted slots or saddles, on which the weight is distributed so that bending moments are reduced and partly due to that much of the fuel is refilled after the rocket is raised to a vertical position. Then the fully assembled rocket, the axis of which is still horizontal, is transferred to the floating structure. The floating structure floats, the distance remaining to the starting position, where the rocket rises to a vertical position and launches.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NO951694A NO951694L (en) | 1995-05-02 | 1995-05-02 | Method of rocket launch |
PCT/NO1996/000103 WO1996034795A1 (en) | 1995-05-02 | 1996-04-30 | Method for rocket launching |
Publications (1)
Publication Number | Publication Date |
---|---|
UA29516C2 true UA29516C2 (en) | 2000-11-15 |
Family
ID=19898168
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
UA97115700A UA29516C2 (en) | 1995-05-02 | 1996-04-30 | method of assembly, preparation, transport to launching site and launching of rockets |
Country Status (10)
Country | Link |
---|---|
US (1) | US5932830A (en) |
JP (1) | JPH11504293A (en) |
KR (1) | KR19990008286A (en) |
AU (1) | AU701314B2 (en) |
BR (1) | BR9608303A (en) |
DE (1) | DE19681370T1 (en) |
GB (2) | GB2315047B (en) |
NO (1) | NO951694L (en) |
UA (1) | UA29516C2 (en) |
WO (1) | WO1996034795A1 (en) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NO301633B1 (en) * | 1996-02-19 | 1997-11-24 | Kvaerner Maritime As | Method of rocket transmission |
NO970952L (en) * | 1997-02-28 | 1998-08-31 | Kvaerner Maritime As | Method and apparatus for counteracting the heel of a vessel |
US6186039B1 (en) * | 1998-02-25 | 2001-02-13 | Kistler Aerospace Corporation | Spacecraft launch system and method |
NL1016859C2 (en) * | 2000-12-13 | 2002-06-14 | Marine Construct B V | Method and device for placing at least one windmill on open water. |
US7900547B2 (en) * | 2008-01-17 | 2011-03-08 | The Boeing Company | System and method for preparing a launch device |
WO2010099228A1 (en) | 2009-02-24 | 2010-09-02 | Blue Origin, Llc | Bidirectional control surfaces for use with high speed vehicles, and associated systems and methods |
US9487308B2 (en) | 2013-03-15 | 2016-11-08 | Blue Origin, Llc | Launch vehicles with ring-shaped external elements, and associated systems and methods |
US10822122B2 (en) | 2016-12-28 | 2020-11-03 | Blue Origin, Llc | Vertical landing systems for space vehicles and associated methods |
CN107524660B (en) * | 2017-08-21 | 2019-08-30 | 北京航天发射技术研究所 | A control method and control system for vertical adjustment of large structural parts |
RU2734036C1 (en) * | 2020-02-18 | 2020-10-12 | Федеральное государственное бюджетное учреждение "Центральный научно-исследовательский испытательный институт инженерных войск имени Героя Советского Союза генерал-лейтенанта инженерных войск Д.М. Карбышева" Министерства обороны Российской Федерации | Fortification structure for missile launchers |
CN112229270B (en) * | 2020-10-13 | 2023-04-25 | 北京航天发射技术研究所 | A launch platform for a splicable mobile launch vehicle |
CN114543591B (en) * | 2022-03-08 | 2023-09-26 | 鲁东大学 | Marine rocket transporting and launching method |
CN114909952B (en) * | 2022-04-20 | 2023-08-18 | 北京航天试验技术研究所 | Foldable movable liquid rocket launching frame |
CN115265271B (en) * | 2022-08-22 | 2023-06-16 | 鲁东大学 | Part processing three-dimensional bin based on pseudo shipment |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3074321A (en) * | 1960-05-23 | 1963-01-22 | Draim John Emery | Transportation of a floatable rocket vehicle |
US3284888A (en) * | 1963-05-09 | 1966-11-15 | Edward J Donnelly | Method and apparatus for assembling and erecting a rocket or missile |
JPH0777880B2 (en) * | 1986-03-12 | 1995-08-23 | 山九株式会社 | Offshore launch system for space rockets |
US4916999A (en) * | 1988-10-27 | 1990-04-17 | Rowan Companies, Inc. | Offshore launching system |
JPH02290799A (en) * | 1989-04-28 | 1990-11-30 | Sankiyuu Kk | Device for transfer mobile type underway rocket launcher on the sea |
US5191162A (en) * | 1991-09-05 | 1993-03-02 | Newport News Shipbuilding And Dry Dock Company | Method and apparatus for a ship-based rocket launching structure |
-
1995
- 1995-05-02 NO NO951694A patent/NO951694L/en unknown
-
1996
- 1996-04-30 UA UA97115700A patent/UA29516C2/en unknown
- 1996-04-30 JP JP8532835A patent/JPH11504293A/en not_active Ceased
- 1996-04-30 DE DE19681370T patent/DE19681370T1/en not_active Withdrawn
- 1996-04-30 WO PCT/NO1996/000103 patent/WO1996034795A1/en not_active Application Discontinuation
- 1996-04-30 US US08/945,504 patent/US5932830A/en not_active Expired - Lifetime
- 1996-04-30 AU AU57055/96A patent/AU701314B2/en not_active Ceased
- 1996-04-30 KR KR1019970707812A patent/KR19990008286A/en not_active Application Discontinuation
- 1996-04-30 GB GB9722240A patent/GB2315047B/en not_active Expired - Fee Related
- 1996-04-30 BR BR9608303A patent/BR9608303A/en not_active IP Right Cessation
-
1997
- 1997-10-20 GB GBGB9721529.7A patent/GB9721529D0/en active Pending
Also Published As
Publication number | Publication date |
---|---|
AU701314B2 (en) | 1999-01-28 |
NO951694L (en) | 1996-11-04 |
NO951694D0 (en) | 1995-05-02 |
DE19681370T1 (en) | 1998-04-02 |
GB9722240D0 (en) | 1997-12-24 |
KR19990008286A (en) | 1999-01-25 |
WO1996034795A1 (en) | 1996-11-07 |
AU5705596A (en) | 1996-11-21 |
BR9608303A (en) | 1999-08-24 |
GB9721529D0 (en) | 1997-12-10 |
JPH11504293A (en) | 1999-04-20 |
US5932830A (en) | 1999-08-03 |
GB2315047A (en) | 1998-01-21 |
GB2315047B (en) | 1999-02-10 |
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